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RU2011110339A - METHOD FOR ASSEMBLING AND FORMING A MULTI-LAYER PANEL FORM - Google Patents

METHOD FOR ASSEMBLING AND FORMING A MULTI-LAYER PANEL FORM Download PDF

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Publication number
RU2011110339A
RU2011110339A RU2011110339/05A RU2011110339A RU2011110339A RU 2011110339 A RU2011110339 A RU 2011110339A RU 2011110339/05 A RU2011110339/05 A RU 2011110339/05A RU 2011110339 A RU2011110339 A RU 2011110339A RU 2011110339 A RU2011110339 A RU 2011110339A
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RU
Russia
Prior art keywords
intermediate element
forming surface
vacuum
multilayer panel
bag
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Application number
RU2011110339/05A
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Russian (ru)
Other versions
RU2516508C2 (en
Inventor
Эндрю ЛЕВЕРС (GB)
Эндрю ЛЕВЕРС
Гари УИЛЕС (GB)
Гари УИЛЕС
Original Assignee
Эйрбас Оперэйшнз Лимитед (Gb)
Эйрбас Оперэйшнз Лимитед
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Publication of RU2011110339A publication Critical patent/RU2011110339A/en
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Publication of RU2516508C2 publication Critical patent/RU2516508C2/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/544—Details of vacuum bags, e.g. materials or shape
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C31/00—Handling, e.g. feeding of the material to be shaped, storage of plastics material before moulding; Automation, i.e. automated handling lines in plastics processing plants, e.g. using manipulators or robots
    • B29C31/04—Feeding of the material to be moulded, e.g. into a mould cavity
    • B29C31/08—Feeding of the material to be moulded, e.g. into a mould cavity of preforms to be moulded, e.g. tablets, fibre reinforced preforms, extruded ribbons, tubes or profiles; Manipulating means specially adapted for feeding preforms, e.g. supports conveyors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1043—Subsequent to assembly
    • Y10T156/1044—Subsequent to assembly of parallel stacked sheets only
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628—Nonplanar uniform thickness material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Table Devices Or Equipment (AREA)

Abstract

1. Способ сборки и придания формы многослойной панели, включающий: установку промежуточного элемента на укладочный стол; сборку пакета путем укладки последовательности слоев на промежуточный элемент на укладочном столе; удаление промежуточного элемента и пакета с укладочного стола и помещение их на формующую поверхность; прижатие пакета к формующей поверхности через промежуточный элемент таким образом, чтобы изменить форму пакета для получения сформованной многослойной панели, и удаление сформованной многослойной панели с промежуточного элемента, причем пакет прижимают к формующей поверхности с помощью разности давлений воздуха, по меньшей мере, частично обеспечиваемой с помощью всасывания, при этом всасывание создают путем укладки вакуумного мешка на пакет на промежуточном элементе и создания частичного вакуума между вакуумным мешком и формующей поверхностью, и при этом способ дополнительно включает в себя прижатие промежуточного элемента к формующей поверхности после удаления вакуумного мешка с помощью создания герметичного уплотнения между промежуточным элементом и вакуум-коробкой для получения вакуумной камеры, причем вакуумная камера содержит формующую поверхность, и создания частичного вакуума в вакуумной камере. ! 2. Способ по п.1, отличающийся тем, что дополнительно включает удаление вакуумного мешка со сформованной многослойной панели; соединение сформованной многослойной панели с одним или более композитных компонентов после удаления вакуумного мешка и совместное отверждение композитного компонента (компонентов) со сформованной многослойной панелью. ! 3. Способ по п.1 или 2, отлича 1. The method of assembly and shaping a multilayer panel, including: installing an intermediate element on a laying table; assembly of the package by laying a sequence of layers on an intermediate element on a laying table; removal of the intermediate element and the package from the laying table and placing them on the forming surface; pressing the bag to the forming surface through the intermediate element so as to change the shape of the package to obtain a molded multilayer panel, and removing the molded multilayer panel from the intermediate element, the package being pressed against the forming surface using an air pressure difference at least partially provided by suction, while suction is created by laying a vacuum bag on a bag on an intermediate element and creating a partial vacuum between the vacuum bag and the forming surface, and the method further includes pressing the intermediate element to the forming surface after removing the vacuum bag by creating a tight seal between the intermediate element and the vacuum box to obtain a vacuum chamber, the vacuum chamber containing the forming surface, and creating a partial vacuum in the vacuum the camera. ! 2. The method according to claim 1, characterized in that it further includes removing the vacuum bag from the molded multilayer panel; connecting the molded multilayer panel with one or more composite components after removing the vacuum bag and curing the composite component (s) together with the molded multilayer panel. ! 3. The method according to claim 1 or 2, excellent

Claims (9)

1. Способ сборки и придания формы многослойной панели, включающий: установку промежуточного элемента на укладочный стол; сборку пакета путем укладки последовательности слоев на промежуточный элемент на укладочном столе; удаление промежуточного элемента и пакета с укладочного стола и помещение их на формующую поверхность; прижатие пакета к формующей поверхности через промежуточный элемент таким образом, чтобы изменить форму пакета для получения сформованной многослойной панели, и удаление сформованной многослойной панели с промежуточного элемента, причем пакет прижимают к формующей поверхности с помощью разности давлений воздуха, по меньшей мере, частично обеспечиваемой с помощью всасывания, при этом всасывание создают путем укладки вакуумного мешка на пакет на промежуточном элементе и создания частичного вакуума между вакуумным мешком и формующей поверхностью, и при этом способ дополнительно включает в себя прижатие промежуточного элемента к формующей поверхности после удаления вакуумного мешка с помощью создания герметичного уплотнения между промежуточным элементом и вакуум-коробкой для получения вакуумной камеры, причем вакуумная камера содержит формующую поверхность, и создания частичного вакуума в вакуумной камере.1. The method of assembly and shaping a multilayer panel, including: installing an intermediate element on a laying table; assembly of the package by laying a sequence of layers on an intermediate element on a laying table; removal of the intermediate element and the package from the laying table and placing them on the forming surface; pressing the bag to the forming surface through the intermediate element so as to change the shape of the package to obtain a molded multilayer panel, and removing the molded multilayer panel from the intermediate element, the package being pressed against the forming surface using an air pressure difference at least partially provided by suction, while suction is created by laying a vacuum bag on a bag on an intermediate element and creating a partial vacuum between the vacuum bag and the forming surface, and the method further includes pressing the intermediate element to the forming surface after removing the vacuum bag by creating a tight seal between the intermediate element and the vacuum box to obtain a vacuum chamber, the vacuum chamber containing the forming surface, and creating a partial vacuum in the vacuum the camera. 2. Способ по п.1, отличающийся тем, что дополнительно включает удаление вакуумного мешка со сформованной многослойной панели; соединение сформованной многослойной панели с одним или более композитных компонентов после удаления вакуумного мешка и совместное отверждение композитного компонента (компонентов) со сформованной многослойной панелью.2. The method according to claim 1, characterized in that it further includes removing the vacuum bag from the molded multilayer panel; connecting the molded multilayer panel with one or more composite components after removing the vacuum bag and curing the composite component (s) together with the molded multilayer panel. 3. Способ по п.1 или 2, отличающийся тем, что герметичное уплотнение создают путем надувания уплотняющего элемента между промежуточным элементом и вакуум-коробкой.3. The method according to claim 1 or 2, characterized in that the hermetic seal is created by inflating the sealing element between the intermediate element and the vacuum box. 4. Способ по п.1 или 2, отличающийся тем, что дополнительно включает изменение формы формующей поверхности для получения измененной формующей поверхности и повторение способа по любому из предшествующих пунктов с применением измененной формующей поверхности.4. The method according to claim 1 or 2, characterized in that it further includes changing the shape of the forming surface to obtain a modified forming surface and repeating the method according to any one of the preceding paragraphs using the modified forming surface. 5. Способ по п.4, отличающийся тем, что формующая поверхность содержит два или более формующих элемента, и форму формующей поверхности изменяют путем замены одного или более формующих элементов на новый формующий элемент другой формы.5. The method according to claim 4, characterized in that the forming surface contains two or more forming elements, and the shape of the forming surface is changed by replacing one or more forming elements with a new forming element of a different shape. 6. Способ по п.1 или 2, отличающийся тем, что каждый из слоев содержит последовательность волокон, пропитанных матрицей.6. The method according to claim 1 or 2, characterized in that each of the layers contains a sequence of fibers impregnated with a matrix. 7. Устройство для сборки и придания формы многослойной панели, содержащее: упругий промежуточный элемент; укладочный стол, который может поддерживать упругий промежуточный элемент, и формующую поверхность, к которой через промежуточный элемент может быть прижат пакет таким образом, чтобы изменить форму пакета для получения сформованной многослойной панели; вакуум-коробку; и уплотняющий элемент для создания герметичного уплотнения между промежуточным элементом и вакуум-коробкой.7. A device for assembling and shaping a multilayer panel, comprising: an elastic intermediate element; a laying table that can support the resilient intermediate element, and a forming surface to which the packet can be pressed through the intermediate element so as to change the shape of the packet to obtain a molded multilayer panel; vacuum box; and a sealing element for creating a tight seal between the intermediate element and the vacuum box. 8. Устройство по п.7, отличающееся тем, что формующая поверхность содержит множество формующих элементов в вакуум-коробке.8. The device according to claim 7, characterized in that the forming surface contains many forming elements in a vacuum box. 9. Устройство по п.8, отличающееся тем, что каждый из формующих элементов имеет основание, контактирующее с полом вакуум-коробки, и формующую верхнюю сторону, определяющую часть формующей поверхности. 9. The device according to claim 8, characterized in that each of the forming elements has a base in contact with the floor of the vacuum box, and a forming upper side defining a part of the forming surface.
RU2011110339/05A 2008-09-04 2009-08-28 Method of sandwiched panel assembly and shaping RU2516508C2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GBGB0816114.3A GB0816114D0 (en) 2008-09-04 2008-09-04 Assembling and shaping laminate panel
GB0816114.3 2008-09-04
PCT/GB2009/051085 WO2010026411A2 (en) 2008-09-04 2009-08-28 Assembling and shaping laminate panel

Publications (2)

Publication Number Publication Date
RU2011110339A true RU2011110339A (en) 2012-10-10
RU2516508C2 RU2516508C2 (en) 2014-05-20

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US (2) US8715561B2 (en)
EP (1) EP2318198B1 (en)
JP (1) JP5475782B2 (en)
KR (1) KR101635070B1 (en)
CN (1) CN102137749B (en)
AT (1) ATE544584T1 (en)
BR (1) BRPI0918218A2 (en)
CA (1) CA2734380C (en)
GB (1) GB0816114D0 (en)
RU (1) RU2516508C2 (en)
WO (1) WO2010026411A2 (en)

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JP5475782B2 (en) 2014-04-16
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